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[paparazzi-commits] [paparazzi/paparazzi] e9ca4d: [rotorcraft] v_adapt:


From: GitHub
Subject: [paparazzi-commits] [paparazzi/paparazzi] e9ca4d: [rotorcraft] v_adapt: limit min/max estimated hove...
Date: Thu, 15 Aug 2013 05:05:22 -0700

  Branch: refs/heads/master
  Home:   https://github.com/paparazzi/paparazzi
  Commit: e9ca4d4f1f11f88c82087bf8270397834f4a914c
      
https://github.com/paparazzi/paparazzi/commit/e9ca4d4f1f11f88c82087bf8270397834f4a914c
  Author: Felix Ruess <address@hidden>
  Date:   2013-08-07 (Wed, 07 Aug 2013)

  Changed paths:
    M sw/airborne/firmwares/rotorcraft/guidance/guidance_v_adpt.h

  Log Message:
  -----------
  [rotorcraft] v_adapt: limit min/max estimated hover throttle

The adaptive vertical filter estimates the ratio of vertical acceleration over 
thrust command.
In effect this will now limit the throttle applied in hover between 20% and 75% 
of max throttle by default.


  Commit: 95871c8d2be0236145143d55bc095f4ba1f93269
      
https://github.com/paparazzi/paparazzi/commit/95871c8d2be0236145143d55bc095f4ba1f93269
  Author: Felix Ruess <address@hidden>
  Date:   2013-08-12 (Mon, 12 Aug 2013)

  Changed paths:
    M sw/airborne/firmwares/rotorcraft/guidance/guidance_v.c

  Log Message:
  -----------
  [rotorcraft] v_adapt: reset while not in_flight


  Commit: fcc3b270ed164cb37b1db9e3cb3d8c2a084cfd82
      
https://github.com/paparazzi/paparazzi/commit/fcc3b270ed164cb37b1db9e3cb3d8c2a084cfd82
  Author: Felix Ruess <address@hidden>
  Date:   2013-08-13 (Tue, 13 Aug 2013)

  Changed paths:
    M conf/firmwares/rotorcraft.makefile
    M conf/firmwares/subsystems/rotorcraft/fdm_jsbsim.makefile
    M conf/settings/control/rotorcraft_guidance.xml
    M sw/airborne/firmwares/rotorcraft/guidance/guidance_v.c
    M sw/airborne/firmwares/rotorcraft/guidance/guidance_v.h
    A sw/airborne/firmwares/rotorcraft/guidance/guidance_v_adapt.c
    A sw/airborne/firmwares/rotorcraft/guidance/guidance_v_adapt.h
    R sw/airborne/firmwares/rotorcraft/guidance/guidance_v_adpt.h

  Log Message:
  -----------
  [rotorcraft] v_adapt: config improvements and refactor

- GUIDANCE_V_ADAPT_INITIAL_HOVER_THROTTLE settable in % with default of 0.3
- GUIDANCE_V_ADAPT_THROTTLE_ENABLED:
  - TRUE by default if GUIDANCE_V_NOMINAL_HOVER_THROTTLE was not defined
  - FALSE by default if only GUIDANCE_V_NOMINAL_HOVER_THROTTLE was set in 
airframe file
    (for backwards compatibily)
- switching between nominal_trottle and the adaptive estimate during operation 
via settings


  Commit: b96785b36f8c896b2f5cfcc3ac11dd8c32296905
      
https://github.com/paparazzi/paparazzi/commit/b96785b36f8c896b2f5cfcc3ac11dd8c32296905
  Author: Felix Ruess <address@hidden>
  Date:   2013-08-13 (Tue, 13 Aug 2013)

  Changed paths:
    M conf/airframes/ardrone2_raw.xml
    M conf/airframes/ardrone2_sdk.xml
    M conf/airframes/examples/lisa_asctec.xml
    M conf/airframes/examples/quadrotor_lisa_m_2_pwm_spektrum.xml
    M conf/airframes/examples/quadrotor_lisa_m_mkk.xml
    M conf/airframes/examples/quadrotor_mlkf.xml
    M conf/airframes/examples/quadshot_asp21_spektrum.xml
    M conf/airframes/examples/stm32f4_discovery_test.xml
    M conf/airframes/fraser_lisa_m_rotorcraft.xml

  Log Message:
  -----------
  [conf] update some airframe examples to GUIDANCE_V_ADAPT changes


  Commit: 96dd3e4ff16d212958dfa9c8d2177374906f3c0c
      
https://github.com/paparazzi/paparazzi/commit/96dd3e4ff16d212958dfa9c8d2177374906f3c0c
  Author: Felix Ruess <address@hidden>
  Date:   2013-08-14 (Wed, 14 Aug 2013)

  Changed paths:
    M sw/airborne/firmwares/rotorcraft/guidance/guidance_v_adapt.c

  Log Message:
  -----------
  [rotorcraft] v_adapt: include generated airframe.h


  Commit: 2091a32bbd268ba62e226db78dbbed37b3ab08b7
      
https://github.com/paparazzi/paparazzi/commit/2091a32bbd268ba62e226db78dbbed37b3ab08b7
  Author: Felix Ruess <address@hidden>
  Date:   2013-08-15 (Thu, 15 Aug 2013)

  Changed paths:
    M conf/airframes/ardrone2_raw.xml
    M conf/airframes/ardrone2_sdk.xml
    M conf/airframes/examples/lisa_asctec.xml
    M conf/airframes/examples/quadrotor_lisa_m_2_pwm_spektrum.xml
    M conf/airframes/examples/quadrotor_lisa_m_mkk.xml
    M conf/airframes/examples/quadrotor_mlkf.xml
    M conf/airframes/examples/quadshot_asp21_spektrum.xml
    M conf/airframes/examples/stm32f4_discovery_test.xml
    M conf/airframes/fraser_lisa_m_rotorcraft.xml
    M conf/firmwares/rotorcraft.makefile
    M conf/firmwares/subsystems/rotorcraft/fdm_jsbsim.makefile
    M conf/settings/control/rotorcraft_guidance.xml
    M sw/airborne/firmwares/rotorcraft/guidance/guidance_v.c
    M sw/airborne/firmwares/rotorcraft/guidance/guidance_v.h
    A sw/airborne/firmwares/rotorcraft/guidance/guidance_v_adapt.c
    A sw/airborne/firmwares/rotorcraft/guidance/guidance_v_adapt.h
    R sw/airborne/firmwares/rotorcraft/guidance/guidance_v_adpt.h

  Log Message:
  -----------
  Merge pull request #495 from flixr/v_adapt_limits

adaptive thrust estimation limits

- GUIDANCE_V_ADAPT_INITIAL_HOVER_THROTTLE settable in % with default of 0.3
- GUIDANCE_V_ADAPT_THROTTLE_ENABLED:
  TRUE by default if GUIDANCE_V_NOMINAL_HOVER_THROTTLE was not defined
  FALSE by default if only GUIDANCE_V_NOMINAL_HOVER_THROTTLE was set in 
airframe file (for backwards compatibility)
- switching between nominal_throttle and the adaptive estimate during operation 
via settings


Compare: 
https://github.com/paparazzi/paparazzi/compare/d15131c0f33c...2091a32bbd26

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